N506DA, cancelled Jul 18, 2002
Service difficulty reports · 61
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N506DA' AND deregistration_id = 'N506DA-2002-07-18' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N506DA' AND deregistration_id = 'N506DA-2002-07-18' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DL72L011689Engine · power lossON TAKEOFF ROLL, N1 ROLLED BACK TO 80 PERCENT, EPR FOLLOWED. THROTTLE PUSHED BACK UP, ROLLED BACK AGAIN. INSPECTED FCU BURNER PRESSURE LINE, OK. SERVICED BELLOWS AND RAN PER PFHB, NO TROUBLE FOUND.SDR DL72L010805Battery Pack · dischargedLEFT FORWARD OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CKS GOOD.SDR DL72L010787Frame · crackedTHE INNER CHORD OF THE FS 1303 FRAME WAS FOUND WITH A 2 INCH LONG CRACK IN THE AFT FLANGE OF THE CHORD. THE CRACK WAS AT A HYDRAULIC LINE CLAMP LOCATION JUST ABOVE THE RT AFT VENTRAL STAIRWAY TORQUE BOX ASSY. THE FLANGE WAS TRIMMED TO REMOVE THE CRACK AND ANSDR DL72L010783Stringer · corrodedFOUND ON B2 LETTER CK CORROSION STR 26L STA 464. REPAIRED PER SRM 53-10-3.SDR DL72L002272Transponder · inoperativeNR 2 ATC TRANSPONDER IS INOP. REPLACED TRANSPONDER PERFORMED TEST PER M/M CHECKS NORMAL.SDR DL72L001973Fitting · crackedROUTINE INSPECTIONS OF THE LT AND RT WING LEADING EDGE SLAT DOWNSTOP FITTINGS REVEALED A BROKEN BOLT IN A FITTING FOR THE NR 6 SLAT. THE CONDITION IS TYPICAL OF BAC S/B 727-57-171AND AD 94-07-08. THE DOWNSTOP FITTINGS OF THE NR 6 SLAT WERE MODIFIED PER THESDR DL72L000549Frame · damagedDURING INSTALLATION OF THE SPLICE REPAIR AND PREVENTATIVE MODIFICATION PER S/B 727-53-0210. MAINTENANCE ENCOUNTERED SHORT FASTENER SPACING AND DISCREPANCIES WITH THE BOEING REWORK DRAWING ERA 334174-14AD ALLOWS 3/16 FASTENERS INSTEAD OF THE 1/4 FASTENSDR DL72L000548Frame · crackedTHE RT FRAME OF THE AFT ENTRY DOOR AT FS 1183 WAS REPAIRED/ MODIFIED PER EO 4-73994-3AD/SB 727-53-0210. DURING THE ACCOMPLISHMENT OF THE MODIFICATION TWO FASTENER HOLES HAD A CRACK INDICATION. ERA 334176-14AD REPAIRED THE HOLES BY OVERSIZING THEM AND INSTSDR DL72L000517Skin · crackedCRACKS WERE FOUND IN THE FUSELAGE SKIN AT STRINGER 4R BETWEEN FS 360 AND FS 480. ERA 334145-14AD REPLACES THE LAP JOINT WITH AN EXTERNAL DOUBLER. THE DAMAGE WAS FOUND AT HMV.SDR DL72L000516Skin · gougedA GOUGE WAS FOUND IN THE SKIN ON THE RIGHT SIDE AT FS 950 AND STRINGER 8 AND WAS REMOVED WITH A 2 X 4.25 CUTOUT. ERA 334199-14 REPAIRS THE DAMAGE WITH AN EXTERNAL DOUBLER SIMILIAR TO THAT OF SRM 53-30-3, FIG 3. THE DAMAGE WAS FOUND AT HMV.SDR DL72L000500Flap Track · corrodedDURING OVERHAUL ON THE I/B FLAP, I/B TRACK ASSY, CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS AND WEAR AT THE FWD ATTACH LUGS AND SPACER BAR HOLES. REPAIRED PER ER/A 387258-14AD AND BF GOODRICH ENGINEERING REPAIR NR 23-0575.SDR DL72L000499Skin · debondedTHE INTERNAL DOUBLER OF THE AFT LAVATORY SERVICE PANEL CUTOUT WAS FOUND TO BE DISBONDED AT AN EXISTING REPAIR. THE SKIN AND DOUBLER WAS CUTOUT AND REMOVED FROM AROUND THE AFT LAV SERVICE PANEL AREA. THE SECTION OF SKIN WAS REPLACED AND SPLICED IN USING AN INSDR DL72L000498Flap Track · corrodedDURING OVERHAUL OF THE I/B FLAP I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS. IN ADDITION, TYPICAL WEAR WAS FOUND AT THE FWD ATTACH LUGS, AND THE MLG DOOR HINGE FITTING ATTACH HOLES, THE SPACER BAR ATTACH HOLES, ANDSDR DL72L000496Skin · lightning strikeNUMEROUS LIGHTNING STRIKES WERE FOUND FROM FS 188 TO FS 259 JUST ABOVE STR 17R. THE DAMAGES WERE EITHER BLENDED OR CUT OUT AND AN EXTERNAL REPAIR WAS INSTALLED PER ERA 334150-14, SIMILAR TO THAT OF SRM REPAIR 53-30-3, FIGURE 3. THE DAMAGE WAS FOUND AT HMV.SDR DL72L000826Angle · crackedDURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 37 INCHES FROM I/B END. THE ANGLE WAS REPAIRED BY SPLICING IN A NEW SECTION OF ANGLE AND INSTALLING A DOUBLER PER MM 57-52-0 FIG 802.SDR DL72L000825Angle · crackedDURING SHOP VISIT, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 23 INCHES FROM I/B END. THE ANGLE WAS REPAIRED BY INSTALLING A NEW SECTION OF ANGLE AND SPLICING IN WITH A DOUBLER PER MM 57-52-0, FIG 802.SDR DL72L000514Rib · crackedAT HMV2 FOUND RIB CRACKED O/B SIDE OF TAI DUCT ON N1 L/E SLAT. FABD DOUBLER PER MM 57-54-0 FIG 814, ALODINED PER PS 900-2-4-1 NR 2, INSTALLED PER MM 57-54-0 FIG 814.SDR DL72L000513Web · crackedAT HMV2 FOUND WEB CRACKED INSIDE VERT STAB AT BOTTOM LT SIDE OF S-DUCT STA 1303. REMOVED STIFFENER FROM STA 1303, STA 1323. FABD REPAIR AND STOPPED DRILLED PER SRM 53-10-4D, CHEM TREAT PER PS 900-2-4-1 NR 2, DYE CKD PER PS 900-6-3 NR 1, REPAIRED PER SRM 53-1SDR DL72L000512Web · crackedAT HMV2 FOUND WEB CRACKED INSIDE VERT STAB AT BOTTOM RT SIDE OF S-DUCT STA 1303. REMOVED NR 2 ANTI ICE DUCT AT STA 1303 - 1280, FABD REPAIR AND STOPPED DRILLED CRACK PER SRM 53-10-4D, CHEM TREATED PER PS 900-2-4-1 NR 2, DYE CKD PER PS 900-6-3 NR 1, INSTALLED SDR DL72L000587Skin · crackedAFT SPAR DOUBLER CRACKED. REPAIRED PER M/M 57-52-0 FIG 802, ON SO 858935.SDR DL72L992253Skin · crackedFUSELAGE SKIN ASSY L1 DOOR CUTOUT, FS 348 LWR AFT CORNER, CRACK REPAIR. THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT (FS 348) WAS FOUND WITH A 4.5 INCH CRACK IN THE SKIN AND BEAR STRAP. THE CRACK WAS CUT OUT OF ALL LAYERS AND AN EXTERNAL DOUBLER AND TRIPLERSDR DL72L990908Skin · crackedFUSELAGE SKIN FS 520-540, STRINGER 26L SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK SDR DL72L990611Indicator · failedOUTBOARD T/E FLAPS DID NOT EXTEND WHEN FLAP LEVER MOVED FROM UP TO 2 DEG. RETURNED LEVER TO UP, RAN THE POM CK LIST. TRAILING EDGE FLAP ABNORMAL ALTERNATE/FLAP EXTENSION ON I/B FLAPS WORKED FINE. CHECKED CABLES AND PULLEYS, ALL CKS OK. REPLACED O/B FLAP POSSDR DL72L990497Skin · crackedTHE VERTICAL STABILIZER SKIN WAS FOUND CRACKED AT FIN STA 42 AT STRINGER 1R BETWEEN RIB 3A AND 4. THE CRACK WAS LOCATED BELOW AN EXISTING REPAIR. THE EXISTING REPAIR WAS REMOVED AND BOTH DAMAGE LOCATIONS INCORPORATED INTO ONE REPAIR PER B727 SRM 55-30-3, FIGSDR DL72L990469Skin · crackedFOUND DURING F-2 LETTER CHECK, .5 INCH CRACK LT ELEVATOR LOWER SKIN FROM RIVET FWD I/B SIDE OF TAB ROD CUTOUT. REPAIRED PER SRM 55-20-3 FIG 4.SDR DL72L990015Power Supply · inopESCAPE PATH LIGHTING INOP ROWS 27 AFT. REPLACED POWER SUPPLY, CKS OK.SDR DL72L982142Support · crackedTHE DOUBLERS FOR THE NR 7 SLAT ACTUATOR SUPPORT STRUCTURE WERE FOUND WITH THE TYPICAL CRACKS PER BAC S/B 727-57-0130, REV 2. THE CRACKED DOUBLERS WERE REPAIRED/MODIFIED PER THE REQUIREMENTS OF THE S/B. THE REPAIR WAS DOCUMENTED PER ER/A 365879-14AD.SDR DL72L981973Trim · out of positionA/C UNABLE TO PRESSURIZE. FOUND A PIECE OF INTERIOR TRIM BETWEEN DOOR SEAL AND A/C FRAME. REPOSITIONED TRIM, ALL OPS NORMAL.SDR DL72L981596Spar · crackedA TYPICAL CRACK WAS FOUND IN THE REAR SPAR OF THE LT ELEVATOR EXTENDING FROM UNDER THE SHEAR PLATE OF THE MIDDLE TAB FITTING. THE CRACK EXTENDS .125 LONG BEYOND THE FITTING. THE CRACK WAS STOP DRILLED PER BAC S/B 727-55-0089 AND WILL BE RE-INSPECTED WITHIN 1SDR DL72L981583Web · crackedFOUND ON F1 LETTER CK, CRACK IN VERTICAL WEB STA 1225 FROM FASTENER HOLE. REPAIRED PER MM 53-11-0.SDR DL72L981476Battery · dischargedRT WING FWD EMER EXT LIGHT WILL NOT LIGHT. REPLACED M655 BATT AND PWR SUPP.SDR DL72L972693Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT STA 1050, S-29R. THE SKIN WAS CUTOUT WITH A 1 X 4 CUTOUT. THE DAMAGE WAS ADJACENT TO A PREVIOUSLY INSTALLED SKIN REPAIR. THE EXISTING REPAIR WAS REMOVED AND A NEW DOUBLER INSTALLED TO INCORPORATE BOTH REPAIR ASDR DL72L972642Skin · gougedFUSELAGE, SKIN FS 340-380 STRINGER 20L-21L : REPAIR FOR SKIN GOUGE AND DENT CUTOUTS. THE FUSELAGE SKIN BETWEEN FS 340 AND 380 AND BETWEEN STRINGER 20L AND 21L WAS BADLY GOUGED AND DENTED. THE DAMAGED AREAS WERE CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER ANSDR DL72L972591Batteries · dischargedEMERGENCY LIGHTS ABOVE BOTTOM OF AFT AIRSTAIRS INOP. REPLACED BATTERIES.SDR DL72L972307Skin · corrodedCORROSION FOUND ON THE INB'D SURFACE OF THE FUSELAGE SKIN AT STA 950F TO 972 AT STGR 28L. REPAIRED PER ERA 330980-14, REV A.SDR DL72L971937Battery Pack · dischargedPER OMI- CK RT FWD CN OVERWING EXIT/EMER LIGHTS. REPLACED BATT PACK, OPN CKS NML.SDR DL72L971910Power Supply · inoperativeAFT SECTION OF E PATH LIGHTING INOP. REPLACED PWR SUPPLY, CKS GOOD.SDR DL72L962338Frame · crackedFOUND ON D-2 LETTER CK, .375 INCH VISIBLE CRACK LT AFT SERVICE DOOR PAN AT UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2.SDR DL72L961099Power Pack · inoperativeFOUND TRACK LIGHTING INOP FROM ROW 27 TO AFT. REPLACED POWER PACK, LIGHTS OPERATED NORMAL.SDR DL72L960642Skin · crackedA .25 INCH CRACK IN COVE SKIN LOWER ATTACH ANGLE BELOW NR 2 SLAT ACTUATOR ROD. FOUND DURING D-1 LETTER CHECK. REPAIRED PER MM 57-54-0.SDR DL72L960641Rib · crackedFOUND DURING D-1 LETTER CHECK, NR 3 L/E SLAT NOSE RIB CRACKED 1 INCH ON I/B AND O/B SIDES. REPAIRED PER MM 57-54-0.SDR DL72L960640Attach Fitting · crackedA .5 INCH CRACK IN NR 1 SLAT ACTUATOR I/B ATTACH FITTING. FOUND DURING D-1 LETTER CHECK. REPAIRED PER MM 57-20-21.SDR DL72L960639Attach Fitting · crackedDURING D-1 LETTER CHECK, FOUND .5 INCH CRACK IN NR 1 SLAT ACTUATOR O/B ATTACH FITTING. REPAIRED PER MM 57-20-21.SDR DL72L954215Battery Pack · dischargedMID CABIN CENTER AISLE AND RT OVERWING EMERGENCY EXIT, EMERGENCY LIGHTS INOP. REPLACED BATTERIES, OPERATION NORMAL.SDR DL72L953881Angle · crackTHERE IS A .3750 CRACK ON THE RIGHT FORWARD AIRSTAIR TORQUE BOX ANGLE AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-0708, WHICH REQUIRES INSPECTION PER S/B 53-0129.SDR DL72L953930Stringer · damagedDURING CV-2 CHECK, STA 990 FRAME WAS CUT TO FACILITATE MTC OF STRINGER 29L REF NR 95. REPAIRED PER M/M 53-12-0 PG 806 AND 807 FIG 805.SDR DL72L953875Web · crackedDURING CV2 CHECK, FOUND .25 INCH CRACK AT LIGHTNING HOLE, INBD VERT WEB RT STA 1225. REPAIRED PER M/M 53-11-0.SDR DL72L953426Angle · crackedA 2 INCH CRACK IN NR 5 SLAT COVE SKIN ATTACH ANGLE O/B END. FOUND DURING C-2 LTR CK. REPAIRED PER MM 57-54-00.SDR DL72L951216Skin · crackedBAY NR 6 INNER SKIN, CRACKED AROUND RIVET. REPAIRED PER MM 57-54-0 FIG 803A. BAY NR 14 DOUBLER CRACKED .5 INCH LONG FWD TOP CORNER (MKD). REPAIRED PER MM 57-54-0 FIG 804 SLAT NR 5. FOUND DURING SHOP INSPECTION.SDR DL72L951076Rib · crackedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH CRACKED RIBS AT LOCATIONS NR 17, 18, 19. REPAIRED PER MM 57-54-0.
Back to N506DA, cancelled Jul 18, 2002